View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66500U 26144.82776672 +.00000000 +00000-0 +67093-3 0 00000
2 66500 43.0005 284.1417 0001099 262.4682 97.6044 15.27591466 03
| Epoch (UTC): | 24 May 2026 19:51:59 |
| Eccentricity: | 0.0001099 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.1417° |
| argument of perigee: | 262.4682° |
| revolutions per day: | 15.27591466 |
| mean anomaly at epoch: | 97.6044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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